[go: up one dir, main page]

US7350425B2 - Method of eliminating hysteresis from a magnetoelastic torque sensor - Google Patents

Method of eliminating hysteresis from a magnetoelastic torque sensor Download PDF

Info

Publication number
US7350425B2
US7350425B2 US11/232,603 US23260305A US7350425B2 US 7350425 B2 US7350425 B2 US 7350425B2 US 23260305 A US23260305 A US 23260305A US 7350425 B2 US7350425 B2 US 7350425B2
Authority
US
United States
Prior art keywords
magnetic field
coil
torque
alternating current
recited
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related, expires
Application number
US11/232,603
Other versions
US20070062312A1 (en
Inventor
David W. Cripe
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Continental Automotive Systems Inc
Original Assignee
Continental Automotive Systems US Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Continental Automotive Systems US Inc filed Critical Continental Automotive Systems US Inc
Priority to US11/232,603 priority Critical patent/US7350425B2/en
Assigned to SIEMENS VDO AUTOMOTIVE CORPORATION reassignment SIEMENS VDO AUTOMOTIVE CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CRIPE, DAVID W.
Publication of US20070062312A1 publication Critical patent/US20070062312A1/en
Assigned to CONTINENTAL AUTOMOTIVE SYSTEMS US, INC. reassignment CONTINENTAL AUTOMOTIVE SYSTEMS US, INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SIEMENS VDO AUTOMOTIVE CORPORATION
Application granted granted Critical
Publication of US7350425B2 publication Critical patent/US7350425B2/en
Assigned to CONTINENTAL AUTOMOTIVE SYSTEMS, INC. reassignment CONTINENTAL AUTOMOTIVE SYSTEMS, INC. MERGER (SEE DOCUMENT FOR DETAILS). Assignors: CONTINENTAL AUTOMOTIVE SYSTEMS US, INC.
Expired - Fee Related legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L3/00Measuring torque, work, mechanical power, or mechanical efficiency, in general
    • G01L3/02Rotary-transmission dynamometers
    • G01L3/04Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft
    • G01L3/10Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating
    • G01L3/101Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means
    • G01L3/102Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means involving magnetostrictive means
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L3/00Measuring torque, work, mechanical power, or mechanical efficiency, in general
    • G01L3/02Rotary-transmission dynamometers
    • G01L3/04Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft
    • G01L3/10Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating
    • G01L3/101Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means
    • G01L3/105Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means involving inductive means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/4902Electromagnet, transformer or inductor

Definitions

  • This invention is generally directed toward a method of eliminating hysteresis in a magnetoelastic torque sensor. More particularly, this invention is a method of removing remanent magnetism outside of a desired magnetic flux path.
  • a magnetoelastic torque sensor utilizes one or more bands of magnetoelastic material supported on a substrate.
  • the magnetoelastic bands possess circumferential remanent magnetization bound by the magnetocrystalline anisotropy of the material.
  • Torque applied to the substrate induces a helical shear stress on the magnetoelastic material that results in a shift of the path of the magnetic field from a circumferential to helical orientation.
  • Axial components of the magnetic field are measured utilizing a magnet field measurement device and are utilized to determine torque.
  • a torque sensor includes a coil assembly that is excited by an alternating current to create a magnetic field that reduces or eliminates undesired magnetic field remanences without disturbing desirable magnetic components within the torque transducer.
  • FIG. 2 is an example cross-sectional view of another torque transducer according to this invention.
  • a circumferential magnetic field schematically shown at 18 is disposed in the magnetoelastic ring material 16 .
  • the circumferential direction of the magnetic field 18 is the neutral or non-torqued state of the torque transducer element 15 .
  • a portion of the magnetic field 18 takes on an axial component and moves away from the circumferential direction.
  • the axial component of the magnetic field 18 is illustrated by arrows indicated at 20 .
  • This axial component 20 of the magnetic field 18 is measured by a magnetometer coil 22 .
  • the magnetometer 22 coil is disposed relative to the transducer element 15 to detect the axial component 20 of the magnetic field 18 .
  • a portion of the axial component 20 of the magnetic field 18 remains.
  • the remaining axial component 20 of the magnetic field 18 distorts the zero position of the torque transducer element 15 resulting in an undesirable hysteresis.
  • the torque transducer assembly 10 includes the magnetometer coil 22 with a plurality of magnet wires 24 coiled coaxially with the torque transducer element 15 .
  • the magnetometer coil 22 is connected to a power source 28 that provides an alternating current 25 .
  • the alternating current 25 excites the coil 22 to produce a magnetic field with alternating peaks.
  • the magnitude and frequency of the alternating current 25 is selected such that it will remove the hysteretic magnetic field component 20 while leaving the circumferential component 18 intact.
  • the alternating current 25 is selected to comprise an amplitude and frequency determined based on the specific material utilized for the torque transducer element 15 .
  • torque transducer element 15 comprised of a 9310 steel alloy
  • a 60-hertz frequency having fifty Oe peak fields is utilized.
  • Such a large alternating current magnetically excites the transducer element 15 to remove axial components 20 of the magnetic field 18 . Removal of the axial component 20 of the hysteretic magnetic field 18 provides for the substantial reduction of zero shift.
  • the torque sensor will operate with a substantial reduction or elimination of hysteresis and thereby provide increased accuracy.
  • a method according to this invention includes the alternating of current amplitudes and frequencies to provide the magnetic field detection function and also to provide the hysteretic magnetic field elimination function.
  • a method steps for removing portions of a magnetic field are indicated at 80 by a schematic block drawing.
  • the method begins with the first application of torque to the substrate shaft 12 as indicated at 82 .
  • the distortion or torque applied to the shaft 12 causes a distortion not only in the shaft 12 but also in the magnetoelastic band 16 .
  • the distortion of the magnetoelastic band 16 is detected by a magnetic field detection device as is indicated at 84 .
  • a portion of the magnetic field that was generated by the torque will remain.
  • the axial component of the magnetic hysteresis can cause a shift in the magnetic field read by the torque transducer element 15 .
  • the coil surrounding the torque transducer element 15 is excited with an alternating current as indicated at 88 .
  • the alternating current is determined to provide the required amplitude and frequency that creates an alternating magnetic field with such peak amplitude that exceeds a substantial fraction of the coercive force of a material.
  • the amplitude of the magnetic field generated by the coil is of an amplitude sufficient to result in the saturation of the core material of the flux-gate devices 62 , The saturation of these devices can be determined by coils immediately surrounding them in the conventional manner of fabrication. Asymmetry of the voltage waveform on the flux-gate coils is indicative of the presence of a magnetic field from the transducer element.
  • the method and devices according to this invention generate increased accuracy for a torque sensor by removing axial components of any magnetic fields that can cause zero shift in torque measurements.

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Power Steering Mechanism (AREA)

Abstract

A method and device for reducing hysteresis in a torque transducer element includes a coil that is excited with an alternating current to produce a magnetic field that saturates the torque transducer element. Magnetic saturation of the torque transducer element is provided by an alternating frequency that exceeds any coercive force of the material. The alternating current is slowly reduced to substantially reduce undesired magnetic field. The coil assembly is excited with an amplitude frequency in such a manner as to remove only those components of the magnetic field that are not desired.

Description

BACKGROUND OF THE INVENTION
This invention is generally directed toward a method of eliminating hysteresis in a magnetoelastic torque sensor. More particularly, this invention is a method of removing remanent magnetism outside of a desired magnetic flux path.
A magnetoelastic torque sensor utilizes one or more bands of magnetoelastic material supported on a substrate. The magnetoelastic bands possess circumferential remanent magnetization bound by the magnetocrystalline anisotropy of the material. Torque applied to the substrate induces a helical shear stress on the magnetoelastic material that results in a shift of the path of the magnetic field from a circumferential to helical orientation. Axial components of the magnetic field are measured utilizing a magnet field measurement device and are utilized to determine torque.
Disadvantageously, once the application of torque on the substrate is discontinued, a remanent portion of the magnetic field remains. The axially-directed remanent magnetic field within the magnetoelastic band causes a shift in a zero point of the torque sensor. The shift of the zero value is commonly known as hysteresis. A known method of eliminating the magnetism within a magnetized body includes placing the structure within an alternating magnetic field with peak amplitude exceeding the coercive force of the material. However, such methods require separate devices that are not available during operation, and remove all magnetic components, even those in the desired circumferential magnetic orientation.
Accordingly, it is desirable to develop a method and device for selectively removing axial hysteretic magnetic remanents, while leaving the desirable circumferential magnetic remanences intact.
SUMMARY OF THE INVENTION
An example method according to this invention provides for the elimination of hysteresis with a torque transducer element by exerting an alternating magnetic field from a coil to remove remanent magnetization along an axis of a shaft of the torque transducer.
A method according to this invention includes supporting a coil axially about a torque transducer. The coil is excited by an alternating current of an amplitude sufficient to create an alternating magnetic field with an amplitude a substantial fraction of the coercive force of the material comprising the torque transducer. The magnetic excitation of the torque transducer provides for the elimination of remanent magnetic fields in the axial direction. By specifically and particularly aligning the coil with the magnetoelastic band of the torque transducer the remanent magnetic field in the axial direction can be removed without disturbing the desirable circumferential magnetic field that is disposed within the band of the transducer.
Accordingly, a torque sensor according to this invention includes a coil assembly that is excited by an alternating current to create a magnetic field that reduces or eliminates undesired magnetic field remanences without disturbing desirable magnetic components within the torque transducer.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a partial cross-sectional view of an example torque transducer according to this invention.
FIG. 2 is an example cross-sectional view of another torque transducer according to this invention;
FIG. 3 is a cross-sectional view of yet another example torque sensor according to this invention;
FIG. 4 is a block diagram illustrating the method step according to this invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring to FIG. 1, a portion of a torque transducer sensor assembly 10 is schematically shown. The torque sensor 10 includes a torque transducer element 15 that comprise a substrate or shaft 12 that supports a magnetoelastic ring 16. The magnetoelastic ring 16 is applied onto the shaft 12 such that torque applied as indicated at 26 to the shaft 12 is communicated to the magnetoelastic ring 16.
A circumferential magnetic field schematically shown at 18 is disposed in the magnetoelastic ring material 16. The circumferential direction of the magnetic field 18 is the neutral or non-torqued state of the torque transducer element 15. During the application of torque 26, a portion of the magnetic field 18 takes on an axial component and moves away from the circumferential direction. The axial component of the magnetic field 18 is illustrated by arrows indicated at 20. This axial component 20 of the magnetic field 18 is measured by a magnetometer coil 22. The magnetometer 22 coil is disposed relative to the transducer element 15 to detect the axial component 20 of the magnetic field 18. However, upon removal of torque applied to the shaft 12, a portion of the axial component 20 of the magnetic field 18 remains. The remaining axial component 20 of the magnetic field 18 distorts the zero position of the torque transducer element 15 resulting in an undesirable hysteresis.
Accordingly, the torque transducer assembly 10 according to this invention includes the magnetometer coil 22 with a plurality of magnet wires 24 coiled coaxially with the torque transducer element 15. The magnetometer coil 22 is connected to a power source 28 that provides an alternating current 25. The alternating current 25 excites the coil 22 to produce a magnetic field with alternating peaks. The magnitude and frequency of the alternating current 25 is selected such that it will remove the hysteretic magnetic field component 20 while leaving the circumferential component 18 intact.
The alternating current 25 is selected to comprise an amplitude and frequency determined based on the specific material utilized for the torque transducer element 15. In one example torque transducer element 15 comprised of a 9310 steel alloy, a 60-hertz frequency having fifty Oe peak fields is utilized. Such a large alternating current magnetically excites the transducer element 15 to remove axial components 20 of the magnetic field 18. Removal of the axial component 20 of the hysteretic magnetic field 18 provides for the substantial reduction of zero shift.
Once torque is released and the hysteretic axial component of the magnetic field 20 is removed, the torque sensor will operate with a substantial reduction or elimination of hysteresis and thereby provide increased accuracy.
It is appreciated that the excitation of the magnetometer coil 22 with a large alternating current 25 could potentially interfere with detection of the magnetic field 18 by the magnetic field detection device or magnetometer. However, a method according to this invention includes the alternating of current amplitudes and frequencies to provide the magnetic field detection function and also to provide the hysteretic magnetic field elimination function.
Referring to FIG. 3, another example torque transducer is indicated at 60 and includes a coil assembly 65 that operates only as the demagnetization function to selectively remove axial hysteretic components of the magnetic field 68. Embedded within the coil assembly 65 are magnet vector detection devices 62 as are known. These magnetic vector detection devices communicate measurements of the magnetic field to control devices 64 as is known. The coil assembly 65 operates to selectively remove the axial components 66 of a magnetic field. The coil assembly 65 of the example torque sensor 60 receives an alternating current indicated at 70 to excite the coil 65 and create a periodic magnetic excitation of an amplitude and frequency determined to remove those undesirable hysteretic components of the magnetic field caused by application of torque 26.
Referring to FIG. 4, a method steps for removing portions of a magnetic field are indicated at 80 by a schematic block drawing. The method begins with the first application of torque to the substrate shaft 12 as indicated at 82. The distortion or torque applied to the shaft 12 causes a distortion not only in the shaft 12 but also in the magnetoelastic band 16. The distortion of the magnetoelastic band 16 is detected by a magnetic field detection device as is indicated at 84. Upon the release of torque as indicated at 86, a portion of the magnetic field that was generated by the torque will remain. The axial component of the magnetic hysteresis can cause a shift in the magnetic field read by the torque transducer element 15. This shift caused by the axial components of the hysteretic magnetic field can be eliminated to improve accuracy of the torque transducer assembly. The coil surrounding the torque transducer element 15 is excited with an alternating current as indicated at 88. The alternating current is determined to provide the required amplitude and frequency that creates an alternating magnetic field with such peak amplitude that exceeds a substantial fraction of the coercive force of a material. The amplitude of the magnetic field generated by the coil is of an amplitude sufficient to result in the saturation of the core material of the flux-gate devices 62, The saturation of these devices can be determined by coils immediately surrounding them in the conventional manner of fabrication. Asymmetry of the voltage waveform on the flux-gate coils is indicative of the presence of a magnetic field from the transducer element.
Accordingly, the method and devices according to this invention generate increased accuracy for a torque sensor by removing axial components of any magnetic fields that can cause zero shift in torque measurements.
Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.

Claims (13)

1. A method of removing hysteretic magnetism from a magnetoelastic torque transducer comprising the steps of:
a) supporting a coil concentrically relative to a magnetoelastic portion of the torque transducer; and
b) exciting the coil with an alternating current of a desired frequency and amplitude to selectively erase a hysteretic magnetic field remanent including removing only axial components of the hysteretic magnetic field remanent.
2. The method as recited in claim 1, wherein the frequency and amplitude are selected to include magnetic field peak amplitude exceeding a coercive force of a material comprising the torque transducer.
3. The method as recited in claim 1, including the step of alternating operation of the coil to remove the hysteretic axial magnetic field.
4. The method as recited in claim 3, wherein the coil comprises the magnetometer and is alternately exited with a detection alternating current with a frequency and amplitude that detects distortions in the magnetic field of the torque transducer, and a removal alternating current with a frequency and amplitude that selectively removes undesired hysteretic magnetic field components.
5. The method as recited in claim 4, further comprising the steps of periodically saturating the coil to generate a distortion signal based on superimposition of an excitation field with the magnetic field generated by the torque transducer.
6. The method as recited in claim 1, including the step of detecting a magnetic field within the torque transducer with a magnetic field sensor disposed within said coil.
7. A method of removing hysteretic magnetism from a magnetoelastic torque transducer comprising the steps of:
a) supporting a coil concentrically relative to a magnetoelastic portion of the torque transducer; and
b) exiting the coil with an alternating current of a desired frequency and amplitude to selectively erase a hysteretic magnetic field remanent while leaving intact circumferential components of a magnetic polarization of the torque transducer.
8. A torque sensor comprising:
a substrate that receives a torque load;
a band of magnetoelastic material supported on said substrate and responsive to the torque load on the substrate by generating a magnetic field indicative of the torque load;
a magnetic field sensor that measures the magnetic field;
a coil disposed about the band of magnetoelastic material that generates an alternating magnetic field that removes only axial orientated portions of a magnetic field remaining in the band of magnetoelastic material; and
a power source for supplying the alternating current to the coil for generating the alternating magnetic field, wherein the vower source supplies a first alternating current that generates periodic magnetic saturation in the torque sensor and a second alternating current that selectively eliminates the axially orientated portions of the magnetic field.
9. The torque sensor as recited in claim 8, wherein axial oriented portions of the magnetic field are removed after torque applied to the substrate is released.
10. The torque sensor as recited in claim 8, wherein said coil is disposed coaxially about said substrate.
11. The torque sensor as recited in claim 8, wherein the coil includes an axial length greater or equal to an axial length of the band.
12. The torque sensor as recited in claim 8, wherein the first alternating current and second alternating current are selectively applied to excite the coil.
13. The torque sensor as recited in claim 8, wherein the coil comprises a first coil and a second coil for detecting the magnetic field within the band.
US11/232,603 2005-09-22 2005-09-22 Method of eliminating hysteresis from a magnetoelastic torque sensor Expired - Fee Related US7350425B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US11/232,603 US7350425B2 (en) 2005-09-22 2005-09-22 Method of eliminating hysteresis from a magnetoelastic torque sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/232,603 US7350425B2 (en) 2005-09-22 2005-09-22 Method of eliminating hysteresis from a magnetoelastic torque sensor

Publications (2)

Publication Number Publication Date
US20070062312A1 US20070062312A1 (en) 2007-03-22
US7350425B2 true US7350425B2 (en) 2008-04-01

Family

ID=37882742

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/232,603 Expired - Fee Related US7350425B2 (en) 2005-09-22 2005-09-22 Method of eliminating hysteresis from a magnetoelastic torque sensor

Country Status (1)

Country Link
US (1) US7350425B2 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080004783A1 (en) * 2006-06-19 2008-01-03 Magna Powertrain Usa, Inc. Dynamic Traction Control System
US20080084261A1 (en) * 2006-10-09 2008-04-10 Mccoy Bryan Wayne Magnetostriction aided switching
US9435708B1 (en) 2015-06-16 2016-09-06 Magcanica, Inc. Devices and methods to enhance accuracy of magnetoelastic torque sensors
US20210270688A1 (en) * 2018-06-28 2021-09-02 Trafag Ag Method, device and arrangement for load measurement on a test object

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7320255B2 (en) * 2005-08-12 2008-01-22 Siemens Vdo Automotive Corporation Torque sensor magnetometer
US7640814B2 (en) * 2005-08-12 2010-01-05 Continental Automotive Systems Us, Inc. Demagnetization-field enhancing magnetometer
DE102014219336B3 (en) * 2014-09-24 2016-01-21 Schaeffler Technologies AG & Co. KG Method and arrangement for measuring a force or a moment with a plurality of magnetic field sensors
CN107110664B (en) 2014-09-26 2020-03-17 伯恩斯公司 System and method for effectively balancing/eliminating magnetic interference in magnetic sensors
DE102021134606A1 (en) 2021-12-23 2023-06-29 Melectric Systems GmbH METHOD AND DEVICE FOR POST-TREATMENT OF MAGNETIC MEASURING ELEMENTS

Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5124648A (en) 1987-08-25 1992-06-23 Analog Devices, Inc. Single winding saturable core magnetometer with field nulling
US5351555A (en) 1991-07-29 1994-10-04 Magnetoelastic Devices, Inc. Circularly magnetized non-contact torque sensor and method for measuring torque using same
US5419207A (en) * 1992-06-01 1995-05-30 Unisia Jecs Corporation Detecting and processing circuitry for magnetostriction type torque sensor
US5696575A (en) 1996-04-23 1997-12-09 Hughes Aircraft Digital flux gate magnetometer
US5889215A (en) * 1996-12-04 1999-03-30 Philips Electronics North America Corporation Magnetoelastic torque sensor with shielding flux guide
US5939881A (en) 1997-11-13 1999-08-17 Raytheon Company High dynamic range digital fluxgate magnetometer
WO1999056099A1 (en) 1998-04-23 1999-11-04 Fast Technology Gmbh Magnetising arrangements for torque/force sensor
US6145387A (en) 1997-10-21 2000-11-14 Magna-Lastic Devices, Inc Collarless circularly magnetized torque transducer and method for measuring torque using same
US6222363B1 (en) * 1999-01-08 2001-04-24 Methode Electronics, Inc. Switch-mode flux-gate magnetometer
US6298467B1 (en) 1998-11-10 2001-10-02 International Business Machines Corporation Method and system for reducing hysteresis effect in SOI CMOS circuits
US6300855B1 (en) 1998-12-21 2001-10-09 The United States Of America As Represented By The Secretary Of The Navy Hysteresis reduction in giant magnetostrictive materials
US6346812B1 (en) 1997-05-13 2002-02-12 Fast Technology Ag Conditioner circuit for magnetic field sensor
WO2002023146A1 (en) 2000-09-12 2002-03-21 Fast Technology Ag. Magnetic torque sensor system
US20020162403A1 (en) * 2001-05-05 2002-11-07 Cripe David W. Magnetoelastic torque sensor
US6516508B1 (en) 1999-11-10 2003-02-11 Siemens Vdo Automotive Corporation Magnetoelastic non-compliant torque sensor and method of producing same
US6776057B1 (en) 1999-08-12 2004-08-17 Abas, Incorporated Magnetized transducer element for torque or force sensor
US6871555B2 (en) 2000-04-17 2005-03-29 Abas, Inc. Magnetic transducer element and method of preparation
EP1752751A1 (en) 2005-08-12 2007-02-14 Siemens VDO Automotive Corporation A magnetometer and torque sensor assembly
US7180311B2 (en) * 2004-05-31 2007-02-20 Yamaha Hatsudoki Kabushiki Kaisha Physical quantity sensing device with bridge circuit and zero point adjusting method

Patent Citations (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5124648A (en) 1987-08-25 1992-06-23 Analog Devices, Inc. Single winding saturable core magnetometer with field nulling
US5351555A (en) 1991-07-29 1994-10-04 Magnetoelastic Devices, Inc. Circularly magnetized non-contact torque sensor and method for measuring torque using same
US5419207A (en) * 1992-06-01 1995-05-30 Unisia Jecs Corporation Detecting and processing circuitry for magnetostriction type torque sensor
US5696575A (en) 1996-04-23 1997-12-09 Hughes Aircraft Digital flux gate magnetometer
US5889215A (en) * 1996-12-04 1999-03-30 Philips Electronics North America Corporation Magnetoelastic torque sensor with shielding flux guide
US6346812B1 (en) 1997-05-13 2002-02-12 Fast Technology Ag Conditioner circuit for magnetic field sensor
US6553847B2 (en) 1997-10-21 2003-04-29 Magna-Lastic Devices, Inc. Collarless circularly magnetized torque transducer and method for measuring torque using the same
US6145387A (en) 1997-10-21 2000-11-14 Magna-Lastic Devices, Inc Collarless circularly magnetized torque transducer and method for measuring torque using same
US5939881A (en) 1997-11-13 1999-08-17 Raytheon Company High dynamic range digital fluxgate magnetometer
WO1999056099A1 (en) 1998-04-23 1999-11-04 Fast Technology Gmbh Magnetising arrangements for torque/force sensor
US6298467B1 (en) 1998-11-10 2001-10-02 International Business Machines Corporation Method and system for reducing hysteresis effect in SOI CMOS circuits
US6300855B1 (en) 1998-12-21 2001-10-09 The United States Of America As Represented By The Secretary Of The Navy Hysteresis reduction in giant magnetostrictive materials
US6222363B1 (en) * 1999-01-08 2001-04-24 Methode Electronics, Inc. Switch-mode flux-gate magnetometer
US6776057B1 (en) 1999-08-12 2004-08-17 Abas, Incorporated Magnetized transducer element for torque or force sensor
US6516508B1 (en) 1999-11-10 2003-02-11 Siemens Vdo Automotive Corporation Magnetoelastic non-compliant torque sensor and method of producing same
US6871555B2 (en) 2000-04-17 2005-03-29 Abas, Inc. Magnetic transducer element and method of preparation
WO2002023146A1 (en) 2000-09-12 2002-03-21 Fast Technology Ag. Magnetic torque sensor system
US6698299B2 (en) 2001-05-05 2004-03-02 Methode Electronics, Inc. Magnetoelastic torque sensor
US20020162403A1 (en) * 2001-05-05 2002-11-07 Cripe David W. Magnetoelastic torque sensor
US7180311B2 (en) * 2004-05-31 2007-02-20 Yamaha Hatsudoki Kabushiki Kaisha Physical quantity sensing device with bridge circuit and zero point adjusting method
EP1752751A1 (en) 2005-08-12 2007-02-14 Siemens VDO Automotive Corporation A magnetometer and torque sensor assembly
US20070034021A1 (en) * 2005-08-12 2007-02-15 Siemens Vdo Automotive Corporation Demagnetization-field enhancing magnetometer

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7491145B2 (en) * 2006-06-19 2009-02-17 Magna Powertrain Usa, Inc. Dynamic traction control system
US7813857B2 (en) 2006-06-19 2010-10-12 Magna Powertrain Usa, Inc. Power transfer assembly with torque sensors and torque control system
US20090082934A1 (en) * 2006-06-19 2009-03-26 Magna Powertrain Usa, Inc. Power Transfer Assembly With Torque Sensors And Torque Control System
US20080004783A1 (en) * 2006-06-19 2008-01-03 Magna Powertrain Usa, Inc. Dynamic Traction Control System
US7456714B2 (en) * 2006-10-09 2008-11-25 Igo, Inc. Magnetostriction aided switching
US20080266036A1 (en) * 2006-10-09 2008-10-30 Mccoy Bryan Wayne Magnetostriction aided switching
US20080084261A1 (en) * 2006-10-09 2008-04-10 Mccoy Bryan Wayne Magnetostriction aided switching
US7880573B2 (en) * 2006-10-09 2011-02-01 Igo, Inc. Magnetostriction aided switching
US9435708B1 (en) 2015-06-16 2016-09-06 Magcanica, Inc. Devices and methods to enhance accuracy of magnetoelastic torque sensors
EP3611487A1 (en) 2015-06-16 2020-02-19 Magcanica, Inc. Devices and methods to enhance accuracy of magnetoelastic torque sensors
US11215523B2 (en) 2015-06-16 2022-01-04 Magcanica, Inc. Devices and methods to enhance accuracy of torque sensors
US20210270688A1 (en) * 2018-06-28 2021-09-02 Trafag Ag Method, device and arrangement for load measurement on a test object
US11821804B2 (en) * 2018-06-28 2023-11-21 Trafag Ag Method, device and arrangement for load measurement on a test object

Also Published As

Publication number Publication date
US20070062312A1 (en) 2007-03-22

Similar Documents

Publication Publication Date Title
US7640814B2 (en) Demagnetization-field enhancing magnetometer
CN108020702B (en) Current measuring device
JP4368797B2 (en) Magnetic field sensor and method of operating magnetic field sensor
JP2566709B2 (en) Torque detecting device and torque measuring method thereof
JP6071460B2 (en) System and method for detecting magnetic noise by applying a switching function to a magnetic field sensing coil
JP5684442B2 (en) Magnetic sensor device
US7350425B2 (en) Method of eliminating hysteresis from a magnetoelastic torque sensor
US4891992A (en) Torque detecting apparatus
JP3645116B2 (en) Magneto-impedance effect micro magnetic sensor
EP2193383B1 (en) Magnetoresistive sensor device and method of processing a signal thereof
CN101192464B (en) Method for cancelling hysteresis of magnetoelastic torque sensor
JP2635714B2 (en) DC bias detection method for transformer core
US7308835B2 (en) Reduction of hysteresis in a magnetoelastic torque sensor
JP2002277522A (en) Magnetic field sensor
US7317314B2 (en) Method for measuring stress/strain using Barkhausen noises
KR102234582B1 (en) Method for operating a magnetostrictive sensor
KR20080043006A (en) How to remove hysteresis from magnetoelastic torque sensor
JP2008145165A (en) Magnetoelastic torque sensor and hysteresis elimination method
JP2004184098A (en) Magnetic sensor element and its manufacturing method
JP3652444B2 (en) Stress measuring device
JPWO2008081569A1 (en) Force and displacement detection method
JP2608498B2 (en) Magnetostrictive torque sensor
JP2009145048A (en) Magnetostrictive torque sensor device, magnetostrictive torque sensor device for electric steering, and calibration method for magnetostrictive torque sensor device
JPH02281116A (en) Strain detecting apparatus
JP2000266619A (en) Torque sensor and device for detecting torque of steering shaft

Legal Events

Date Code Title Description
AS Assignment

Owner name: SIEMENS VDO AUTOMOTIVE CORPORATION, MICHIGAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:CRIPE, DAVID W.;REEL/FRAME:017028/0661

Effective date: 20050922

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

AS Assignment

Owner name: CONTINENTAL AUTOMOTIVE SYSTEMS US, INC., MICHIGAN

Free format text: CHANGE OF NAME;ASSIGNOR:SIEMENS VDO AUTOMOTIVE CORPORATION;REEL/FRAME:020493/0471

Effective date: 20071203

STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

AS Assignment

Owner name: CONTINENTAL AUTOMOTIVE SYSTEMS, INC., MICHIGAN

Free format text: MERGER;ASSIGNOR:CONTINENTAL AUTOMOTIVE SYSTEMS US, INC.;REEL/FRAME:033034/0225

Effective date: 20121212

FPAY Fee payment

Year of fee payment: 8

FEPP Fee payment procedure

Free format text: MAINTENANCE FEE REMINDER MAILED (ORIGINAL EVENT CODE: REM.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

LAPS Lapse for failure to pay maintenance fees

Free format text: PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362

FP Lapsed due to failure to pay maintenance fee

Effective date: 20200401